View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 15772U 26071.15781270 +.00000000 +00000-0 +86156-4 0 00002
2 15772 71.1062 82.5137 0033133 124.0851 304.8946 14.21983108 02
| Epoch (UTC): | 12 March 2026 03:47:15 |
| Eccentricity: | 0.0033133 |
| inclination: | 71.1062° |
| perigee height: | 795 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 82.5137° |
| argument of perigee: | 124.0851° |
| revolutions per day: | 14.21983108 |
| mean anomaly at epoch: | 304.8946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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